Axisymmetric bluff-body drag reduction through geometrical modification
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45158
Reference34 articles.
1. Drag-Reducing Techniques for Axi-Symmetric Bluff Bodies
2. Subsonic axisymmetric base flow experiments with base modifications
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